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Gravitation Test - 24

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Gravitation Test - 24
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  • Question 1
    1 / -0
    What is the percentage decrease in the weight of  a body when it is taken 32 km below the surface of the earth? [Radius of the earth=6400km]
    Solution

  • Question 2
    1 / -0
    The value of $$'g'$$ at a depth of $$80 km$$ will be (Radius of earth $$= 6400 km$$ and value of $$'g'$$ on the surface of earth is $$10m/s^2$$)
    Solution
    Let $$g'/ge$$ the acceleration due to gravity in mins
    Then $$g'=g\left(1\times \cfrac {d}{R}\right)=9.8\left(1-\cfrac {640}{6400}\times 10^3\right)$$
    $$=9.8 \times 0.9999m/s^2$$
    $$=9.799m/s^2$$
  • Question 3
    1 / -0
    The value of gravitational constant depends upon : 
    Solution
    The gravitational constant is a universal constant. It remains as it is in any condition. 
    It does not depend on any of the factors like the temperature, mass, distance between the masses.

     Value of G is $$ 6.67 \times 10^{-11} \, Nm^2 kg^{-2} $$ 
  • Question 4
    1 / -0
    A body has weight (W) on the ground. The work which must be done to lift it to a height equal to the radius of the earth, R, is
    Solution
    If acceleration due to gravity was constant, constant force W was to be applied.
    However, due to the decrease in g we need to apply less force as we go higher.
    Hence the work done is lesser.
  • Question 5
    1 / -0
    The ratio of the radius of a planet A to that of planet B is $$r$$. The ratio of accelerations due to gravity for the two planets is $$x$$. The ratio of the escape velocities from the two planets is :
    Solution
    Escape Velocity is given by: $$V_{e}=\sqrt{2gR}$$
    Given: $$ \dfrac{R_A}{R_B} = r$$  and $$\dfrac{g_A}{g_B} = x $$
    Taking ratio of the escape velocities of the $$2$$ planets:
    $$\dfrac{V_A}{V_B} = \sqrt{rx}$$
  • Question 6
    1 / -0
    Consider Earth to be a homogeneous sphere. Scientist A goes deep down in a mine and scientist B goes high up in a balloon. The gravitational field measured by
    Solution
    The variation of 'g' with altitude is: $$g' = g(1- \dfrac{2h}{R})$$
    The variation of 'g' with depth is: $$g' = g(1- \dfrac{d}{R})$$
    So, from the above equations we can deduce that if a person goes deep into a mine or to a height above the Earth's surface, the gravitational field decreases at different rates.
  • Question 7
    1 / -0
    The ratio of acceleration due to gravity at a depth $$h$$ below the surface of earth and at a height $$h$$ above the surface for $$h<<R$$
    Solution

    Acceleration due to gravity at a depth $$h$$ below the surface of earth is

    $$g_d = g(1 - \dfrac{h}{R})$$

    Acceleration due to gravity at a height $$h$$ above the surface of earth is

    $$g_h = g(1- \dfrac{2h}{R})$$

    where, $$g$$ is the acceleration due to gravity on the surface and $$R$$ is the radius of earth.

    So, $$\dfrac{g_d}{g_h} = \dfrac{(R - h)}{ (R - 2h)}$$

    Since $$R>> h$$

    We can conclude that this ratio is constant.

  • Question 8
    1 / -0
    If $$R$$ is radius of the earth and $$W$$ is work done in lifting a body from the ground to an altitude $$R$$, the work which should be done in lifting it further to twice that altitude is:
    Solution
    Work done is equal to change in PE.

    $$W = - \Delta U = U_1-U_2 = -\dfrac{GMm}{R}-(- \dfrac{GMm}{2R}) = -\dfrac{GMm}{2R}$$

    Work done in lifting body from $$2R$$ to $$4R$$.

    $$W' = - \Delta U = U_1-U_2 = -\dfrac{GMm}{2R}-(- \dfrac{GMm}{4R}) = -\dfrac{GMm}{4R} =\dfrac{W}{2}$$
  • Question 9
    1 / -0
    A space craft is launched in a circular orbit very close to the earth. What additional velocity should be given to the space craft so that it might escape the earth's gravitational pull:
    Solution
    Since the spacecraft is moving very close to the surface of earth, we assume its orbital radius to be R(the radius of the earth); implying its current orbital velocity is: $$V_{o}\, = \sqrt{gR}$$.
    But by definition of escape velocity, we know that to escape the surface of earth, the speed required is $$V_{e}\, = \sqrt{2gR}$$.
    Hence, the additional speed to be given to the spacecraft is $$V_{e}\, -\, V_{o}$$.
    Using $$g=9.81$$ and $$R=6400\ km$$, we get the required additional speed as $$3.25km\, s^{-1}$$.
  • Question 10
    1 / -0
    A particle hanging from a spring stretches it by $$1 cm$$ at earth's surface. Radius of earth is $$6400 km$$. At a place $$800 km$$ above the earths surface, the same particle will stretch the spring by
    Solution
    as, $$mg=kx$$
    where, $$x=1cm, k=$$spring constant
    for second case $$mg'=kx'$$
    Hence $$ \dfrac{g}{g'}=\dfrac{x}{x'}$$
    $$x'=xg'/g$$
    $$x'=\dfrac{xgR^2}{(R+h)^2 g}$$
    Earth's radius, $$R=6400$$
    At height, $$h=800$$
    $$x'=\dfrac{1\times (6400 \times 10^3)^2}{(7200 \times 10^3)^2}$$
    $$x'=0.79 cm$$
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